CN104185241B - Suitable for the method for routing of tethered satellite network - Google Patents
Suitable for the method for routing of tethered satellite network Download PDFInfo
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- CN104185241B CN104185241B CN201410452446.8A CN201410452446A CN104185241B CN 104185241 B CN104185241 B CN 104185241B CN 201410452446 A CN201410452446 A CN 201410452446A CN 104185241 B CN104185241 B CN 104185241B
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
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Abstract
The invention discloses a kind of method for routing suitable for tethered satellite network.Use each satellite node of this method, for other satellite nodes in a manner of " storage carries forwarding ", data relay services are provided, under the severe network environments such as satellite node failure, the frequent interruption of inter-satellite link in preset ratio (or predetermined number), the periodically mobile communication opportunity formed of intermediate, satellite node can be utilized, realizes hop-by-hop transmission of the packet between source/destination satellite node.
Description
Technical field
The present invention relates to satellite communication field, more particularly to the satellite node failure of preset ratio (or predetermined number), star
Between link the satellite network method for routing under adverse circumstances such as frequently interrupt.
Background technology
Satellite network is the important component of national information infrastructure, and it is logical to carry emergency disaster relief, Scientific Exploration etc.
Trust business, huge application prospect is possessed in civil and military field.
In occupation of critical role in Satellite Networking, it directly determines the transmittability of satellite network, led to route technology
Believe efficiency and service quality.In order to solve satellite network routing issue, researcher both domestic and external successively proposes a series of
Technical scheme, including, it is explicit multi-path routing algorithms (Compact Explicit Multi-path Routing, CEMR), general
Rate Routing Protocol (Probabilistic Routing Protocol, PRP), auxiliary positioning On-demand routing algorithm (Location-
Assisted On-demand Routing, LAOR), datagram routing algorithm (Datagram Routing Algorithm,
DRA), multilayer satellite routing algorithm (Multi-Layered Satellite Routing Algorithm, MLSR), satellite point
Group Routing Protocol (Satellite Grouping and Routing Protocol, SGRP), layering satellite routing algorithm
(Hierarchical Satellite Routing Protocol, HSRP) etc..Although these existing methods can be competent at typically
Router tasks in satellite network, but because of them completely based on same network topology it is assumed that it is, (1) satellite
The dynamic change of network topology structure is predictable；(2) unexpected link down, the probability of node failure of occurring is very low, with
Cause can be ignored, so larger limitation in application be present, for defending for preset ratio (or predetermined number)
Satellite Networking problem under the severe network environments such as the frequent interruption of star node failure, inter-satellite link is helpless.
The content of the invention
Technical problem to be solved of the embodiment of the present invention is：How preset ratio (or predetermined number) satellite node
Failure, inter-satellite link frequently interrupt etc. realizes satellite network route technology under severe network environment, complete from source satellite node to
The packet transmission of purpose satellite node.
The technical solution used in the present invention is：
A kind of method for routing suitable for tethered satellite network is proposed, it is comprised the concrete steps that：
To during the transmission packet of purpose satellite node, 1. the first satellite node for receiving the packet is caching source satellite node
It is middle to store the packet and carry track movement of the packet according to itself；Set the first satellite node and carry defending for packet to be current
Star node；
2. the current satellite node for carrying packet goes out next-hop satellite node using tethered satellite forwarded algorithms selection,
And at the time of the current satellite node for carrying packet meets with next-hop satellite node, the current satellite node for carrying packet will
Next-hop satellite node is given in the packets forwarding；
If 3. the next-hop satellite node is purpose satellite node, packet transmission is completed；Otherwise, the next-hop is defended
Star node sets is the current satellite nodes for carrying packet and are transferred to step 2..
Wherein, described step 2. in, use the specific of tethered satellite forwarded algorithms selection next-hop satellite node
Step is：
21 in predetermined period, and the current satellite node for carrying packet is according to initial primary topology and forwarding statistical information
Link-state metric value is generated for its each outbound, and then uses Link State distribution method by the link-state metric
Value is diffused into whole tethered satellite network；
22 when needing to select next-hop, and the current satellite node for carrying packet is by the link-state metric value that receives
Set, is spliced into satellite network topological view, next-hop then is calculated on the topological view using dijkstra's algorithm
Satellite node.
Wherein, the initial primary topology in described step 21 is that satellite node obtains from earth station, the initial topology
The period that structure is in open mode by each outbound of satellite node forms.
Wherein, in described step 21, the current satellite node for carrying packet is according to initial topology knot in predetermined period
Structure and forwarding statistical information are that each outbound generates comprising the concrete steps that for link-state metric value：
The 2101 current satellite nodes for carrying packet press predetermined period, on the basis of initial primary topology, with reference to itself
The packets forwarding situation of record, update the forwarding statistical information of each outbound；
The 2102 current satellite nodes for carrying packet will forward statistical information input negative exponential function to obtain each outbound
Link-state metric value.
Wherein, in described step 2102, forwarding statistical information is put down by link connected probability, link transmission ability, link
The energy value that the equal stand-by period points to satellite with link is added to obtain through assigning power.
Wherein, in described step 21, link-state metric value is diffused into limited defend using Link State distribution method
StarNet's network comprises the concrete steps that：
Link-state metric value is packaged into link-state information by the 2111 current satellite nodes for carrying packet, and with chain
Line state information is that list item generates link-state list；
When other satellite nodes in the 2112 current satellite nodes and network for carrying packet meet, they are exchanged respectively immediately
From link-state list；
The 2113 current satellite nodes for carrying packet update the Link State of itself according to the link-state list received
Table.
Wherein, the link-state information in described step 2111 include sequence number, link starting satellite node identification,
The node identification and link-state metric value of link termination satellite.
Wherein, described step 2113 comprises the concrete steps that：
If the inter-satellite link not occurred in itself link-state list in 211301 link-state lists received be present, that
Need to be added to Link State list item corresponding to the link in the link-state list of itself；
If the Link State list item of some links in 211302 link-state lists received, compared with itself link-state list
The Link State list item of middle same link is new, then needs to use new Link State list item to substitute in itself link-state list
Respective links link list item；
If in 211303 link-state lists received, i.e., in the absence of emerging inter-satellite link, Link State list item
Also it is not new, then directly to abandon the link-state list received.
For the present invention compared with background technology, the present invention mainly has advantages below：
(1) each satellite node provides data relay services in a manner of " storage-carrying-forwarding " for other satellite nodes,
Therefore method for routing disclosed by the invention is used, even in the case of whole satellite network not full-mesh, also has and greatly may be used very much
Can, between two satellite nodes in the absence of route path, realize the indirect, reliable of packet, high efficiency of transmission.
(2) in tethered satellite forwarded algorithm, link connected probability, link transmission ability, link have been taken into full account
Average latency and link point to the energy value of satellite, therefore method for routing disclosed by the invention, not only to equipment fault, letter
Satellite network communications environmental catastrophe caused by the interim factor such as road change, malicious sabotage has stronger adaptability and robustness,
And possess load balancing and Energy-aware ability, it can effectively extend satellite network life cycle.
Brief description of the drawings
Fig. 1 is tethered satellite network route method schematic diagram.
Embodiment
Below, with reference to Figure of description 1, the invention will be further described.
Tethered satellite network refers to, the satellite of preset ratio (such as more than 30%) or predetermined number (being greater than 20)
The satellite network of node cisco unity malfunction；Or, due to the reasons such as equipment fault, channel variation, malicious sabotage, inter-satellite link frequency
The satellite network of numerous interruption.
According to one embodiment of present invention, specific embodiment is as follows：
1. tethered satellite network route method overall plan
Each satellite node provides data relay services in a manner of " storage-carrying-forwarding " for other nodes, utilizes centre
The periodically mobile communication opportunity formed of satellite node, realize hop-by-hop transmission of the packet between source/destination node.Specifically
Ground：
(1) when source satellite node will be sent to purpose satellite node to be grouped, the first satellite node of the packet is received,
The packet is stored in the buffer, and carries the packet and is moved according to the track of itself, and sets the first satellite node currently to take
Satellite node with packet.
(2) after next-hop satellite node is gone out using tethered satellite forwarded algorithms selection, carry what is be grouped current
At the time of satellite node meets with next-hop satellite node, the current satellite node for carrying packet forwards the packet to next-hop
Satellite node.
(3) if next-hop satellite node is purpose satellite node, packet transmission is completed；Otherwise, next-hop satellite node
Continue to forward the packet according to the first satellite node identical method, next-hop satellite node is set as that current carry is grouped
Satellite node, and be transferred to step (2).
Fig. 1 gives one embodiment of the method for routing, and (three subgraphs represent t respectively1, t2, t3The network at moment is opened up
Flutter).Wherein, S is source satellite node, and D is purpose satellite node, and 1,2,3,4 is four intermediate, satellite nodes.Assuming that all nodes
All it is periodically mobile, and is ready the packet for forwarding other satellite nodes to send, then, 1. in t1Moment, satellite S
Plan to send data P to satellite D, communication path is not present because S and D is located at different connected domains, between them, so satellite
S judged according to certain tactful (such as the tethered satellite network topology configuration method that will be introduced hereinafter), and according to judgement
As a result, data P is sent to the satellite 2 contacted with it.Because satellite 2 also without reach D route path, it
The data storage P in internal memory, and carry P and move together, to wait transmission opportunity.2. in t2Moment, satellite 2 start same satellite 4
Contact, it is judged also according to certain strategy, it is assumed that result of determination thinks that satellite 4 is most suitable next-hop node, that
Data P is transmitted to satellite 4 by satellite 2.Satellite 4 continues to move together with P.3. in t3At the moment, satellite 4 contacts with D, by P
Hand to D.
2. tethered satellite forwarded algorithm
In predetermined period, satellite node is its each outbound according to initial primary topology and forwarding statistical information
Link-state metric value is generated, and then the link-state metric value is diffused into whole be limited using Link State distribution method and defended
StarNet's network.When needing satellite node to select next-hop, the satellite node can be spelled by the link-state metric value set received
Complete satellite network topological view is picked out, is then calculated using dijkstra's algorithm on the satellite network topological view
Next-hop satellite node.Because Dijkstra is classical graph-theoretical algorithm, its principle is repeated no more.Tethered satellite net is given below
One embodiment of network forwarding algorithm.
(1) initial primary topology
Satellite node can obtain initial primary topology from earth station, and the initial primary topology respectively exports chain by satellite node
Road is in the period composition of open mode.
For example, earth station the initial primary topology of tethered satellite network can be expressed as weighted and directed diagraph G=(V, E,
ωB), wherein, 1. vertex set V represents the satellite node set in network.2. side collection E represents the directed link collection between satellite
Close, include ISL (Inter Satellite Link) satellite links and IOL (Inter Orbit Link) satellite link.③ωB
For representing that isl cycle beats the time varying characteristic of opening/closing, the topology caused by describing satellite node cycle movement is moved
State property.ForThe initial tax weights for making link i → j are ωi→j（t)∈ωB, then can be obtained by formula (1)
ωi→j(t) value.In formula (1),Represent that link i → j can be used for the time for sending data
Section, is precalculated by earth station.
Earth station can be by G=(V, E, ωB）Send every satellite in tethered satellite network to, can also be only by G
Partial information send each satellite to.For example, for any one satellite i in G, earth station only sends information ω to iti→j
(t), i → j ∈ E, the implementation for neither influenceing subsequent technology scheme, the storage resource that can effectively save on satellite again are so done.
(2) link-state metric value
Described using link-state metric value caused by the enchancement factors such as equipment fault, interim environmental change, malicious attack
Satellite network topological dynamics, satellite node update the forwarding of each outbound according to predetermined period (for example, 20 seconds or 100 seconds)
Statistical information, the link-state metric value that statistical information input negative exponential function will be forwarded to obtain each outbound.
For example, forNote satellite link i → j ∈ moment k link-state metric value isForwarding statistical information beThen have：
1) statistical information is forwarded
Forwarding statistical information has various definitions mode, for example, can be by link connected probability, link transmission ability, link
The energy value that average latency points to satellite with link is added to obtain the forwarding statistical information of satellite outbound by assigning power,
Specifically, forRemember that link capability parameters of the satellite link i → j ∈ E in moment k isThen have：
Wherein, α, β, γ andIt is four adjustment factors, their value can specifically be set according to actual conditions, only be needed
Meet conditionAnd.Parameter Pi→j(k)、Qi→j(k)、Ei→j(k) and
Ej(k) physical significance is respectively, 1. Pi→j(k) link i → j connected probability is represented, it is, in the periodIn, link i → j history connection situation.②Qi→j(k) link capability is represented, it is,
Link i → j " bandwidth-Lifetime " product.③Ti→j(k) represent that link i → j is switched to " open shape by " closed mode "
The average latency of state ".④Ej(k) energy value of satellite (such as j in link i → j) pointed by one way link is represented.
It is worth noting that, calculating Pi→j(k)、Qi→j(k)、Ti→jAnd E (k)j(k) during, it is always necessary to use
The initial primary topology of each satellite node is sent to by earth station.
(3) Link State distribution method
First, link-state metric value is packaged into link-state information by satellite node.
Secondly, each satellite node generates link-state list by list item of link-state information.
Again, when satellite node and other satellite nodes meet, they need to exchange respective link-state list immediately.
Finally, after completion of the exchange, the satellite node for participating in exchanging updates itself according to the link-state list received
Link-state list.
1) link-state information
Link-state information can be originated the node mark of the node identification of satellite, link termination satellite by sequence number, link
Know, link-state metric value composition, as shown in formula (4).
LSI=（Seq, src, dst, metric) (4)
Wherein, src is the mark of inter-satellite link starting satellite node；Dst is the mark that inter-satellite link terminates satellite node；seq
It is sequence number, represents the newness degree of the link-state information.Metric is to originate the Link State that satellite node src is monitored
Metric.
2) link state update method
The mode that satellite node updates itself link-state list has a variety of, and a kind of specific method is given below：A) first, such as
Inter-satellite link i → the j not occurred in itself link-state list in the link-state list that fruit receives be present, then need link
Link State list item corresponding to i → j, it is added in the link-state list of itself.If b) second, the link-state list received
In some links Link State list item, the Link State list item compared with same link in itself link-state list is new, then need
New Link State list item is used to substitute the link list item of the respective links in itself link-state list.If c) third, phase
For the link-state list in this node, in the link-state list received, i.e., in the absence of emerging inter-satellite link, link
State list item is not also new, then directly abandons the link-state list received.
Claims (6)
1. a kind of method for routing suitable for tethered satellite network, it is characterised in that methods described comprises the concrete steps that：
1. source satellite node to during the transmission packet of purpose satellite node, deposit in the buffer by the first satellite node for receiving the packet
Store up the packet and carry the packet and moved according to the track of itself；The first satellite node is set as the current satellite section for carrying packet
Point；
2. the current satellite node for carrying packet goes out next-hop satellite node using tethered satellite forwarded algorithms selection, and
At the time of the current satellite node for carrying packet meets with next-hop satellite node, the current satellite node for carrying packet is by this point
Group is transmitted to next-hop satellite node；
If 3. the next-hop satellite node is purpose satellite node, packet transmission is completed；Otherwise, by the next-hop satellite section
Point is set as the current satellite node for carrying packet and is transferred to step 2.；
Described step 2. in, use comprising the concrete steps that for tethered satellite forwarded algorithms selection next-hop satellite node：
21 in predetermined period, and it is it currently to carry the satellite node being grouped according to initial primary topology and forwarding statistical information
Each outbound generation link-state metric value, and then spread the link-state metric value using Link State distribution method
To whole tethered satellite network；
22 when needing to select next-hop, and the current satellite node for carrying packet is by the link-state metric value collection that receives
Close, be spliced into satellite network topological view, next-hop then, which is calculated, on the topological view using dijkstra's algorithm defends
Star node；
In described step 21, the current satellite node for carrying packet is united according to initial primary topology and forwarding in predetermined period
Meter information is that each outbound generates comprising the concrete steps that for link-state metric value：
The 2101 current satellite nodes for carrying packet press predetermined period, on the basis of initial primary topology, with reference to self record
Packets forwarding situation, calculate some forwarding statistical parameters, to it is described it is some forwarding statistical parameters carry out assign power addition obtain simultaneously
Update the forwarding statistical information of each outbound；
The 2102 current satellite nodes for carrying packet will forward statistical information input negative exponential function to obtain the chain of each outbound
Line state metric.
2. it is applied to the method for routing of tethered satellite network as claimed in claim 1, it is characterised in that in described step 21
Initial primary topology be that satellite node obtains from earth station, the initial primary topology is in by each outbound of satellite node
The period composition of open mode.
3. it is applied to the method for routing of tethered satellite network as claimed in claim 1, it is characterised in that some forwarding systems
Counting parameter includes the energy value that link connected probability, link transmission ability, link average latency and link point to satellite.
4. it is applied to the method for routing of tethered satellite network as claimed in claim 1, it is characterised in that described step 21
In, link-state metric value is diffused into tethered satellite network using Link State distribution method and comprised the concrete steps that：
Link-state metric value is packaged into link-state information by the 2111 current satellite nodes for carrying packet, and with Link State
Information is that list item generates link-state list；
When other satellite nodes in the 2112 current satellite nodes and network for carrying packet meet, they exchange respective immediately
Link-state list；
The 2113 current satellite nodes for carrying packet update the link-state list of itself according to the link-state list received.
5. it is applied to the method for routing of tethered satellite network as claimed in claim 4, it is characterised in that described step 2111
In link-state information include sequence number, link starting satellite node identification, the node identification and chain of link termination satellite
Line state metric.
6. it is applied to the method for routing of tethered satellite network as claimed in claim 4, it is characterised in that described step 2113
Comprise the concrete steps that：
If the inter-satellite link not occurred in itself link-state list in 211301 link-state lists received be present, then need
It is added to Link State list item corresponding to the link in the link-state list of itself；
If the Link State list item of some links in 211302 link-state lists received, compared with phase in itself link-state list
Link State list item with link is new, then needs to use new Link State list item to substitute pair in itself link-state list
Answer the link list item of link；
If in 211303 link-state lists received, i.e., in the absence of emerging inter-satellite link, Link State list item is not yet
Newly, then directly abandon the link-state list received.
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| CN104869017B (en) * | 2015-04-30 | 2017-05-31 | 北京空间飞行器总体设计部 | A Kernel Product-Based Topology Optimization Method for Satellite Information System |
| CN110896557B (en) * | 2019-12-23 | 2020-11-27 | 北京邮电大学 | Satellite communication routing method and device |
| CN114095971B (en) * | 2022-01-19 | 2022-05-10 | 浙江吉利控股集团有限公司 | Method, system, device, equipment and storage medium for processing communication data packet |
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